DE2842047C2 - Vorrichtung zur Verteilung von Kraftstoff in einem Nachverbrennungs-Kanal, insbesondere eines Strahltriebwerks - Google Patents

Vorrichtung zur Verteilung von Kraftstoff in einem Nachverbrennungs-Kanal, insbesondere eines Strahltriebwerks

Info

Publication number
DE2842047C2
DE2842047C2 DE2842047A DE2842047A DE2842047C2 DE 2842047 C2 DE2842047 C2 DE 2842047C2 DE 2842047 A DE2842047 A DE 2842047A DE 2842047 A DE2842047 A DE 2842047A DE 2842047 C2 DE2842047 C2 DE 2842047C2
Authority
DE
Germany
Prior art keywords
openings
channel
injection
ring
injection line
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE2842047A
Other languages
German (de)
English (en)
Other versions
DE2842047A1 (de
Inventor
Jean-Claude-Marius Arliguie
Marc Francois Bernard Le Mee Sur Seine Buisson
Jaques Emile Jules Dammarie Les Lys Caruel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE2842047A1 publication Critical patent/DE2842047A1/de
Application granted granted Critical
Publication of DE2842047C2 publication Critical patent/DE2842047C2/de
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Gas Burners (AREA)
DE2842047A 1977-09-27 1978-09-27 Vorrichtung zur Verteilung von Kraftstoff in einem Nachverbrennungs-Kanal, insbesondere eines Strahltriebwerks Expired DE2842047C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7728981A FR2404111A1 (fr) 1977-09-27 1977-09-27 Dispositif de distribution de carburant

Publications (2)

Publication Number Publication Date
DE2842047A1 DE2842047A1 (de) 1979-04-12
DE2842047C2 true DE2842047C2 (de) 1987-05-07

Family

ID=9195798

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2842047A Expired DE2842047C2 (de) 1977-09-27 1978-09-27 Vorrichtung zur Verteilung von Kraftstoff in einem Nachverbrennungs-Kanal, insbesondere eines Strahltriebwerks

Country Status (3)

Country Link
US (1) US4280324A (un)
DE (1) DE2842047C2 (un)
FR (1) FR2404111A1 (un)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2551500B1 (fr) * 1983-09-07 1985-11-08 Snecma Anneau-bruleur pour postcombustion de moteur a reaction
US5150570A (en) * 1989-12-21 1992-09-29 Sundstrand Corporation Unitized fuel manifold and injector for a turbine engine
US5685140A (en) * 1995-06-21 1997-11-11 United Technologies Corporation Method for distributing fuel within an augmentor
US5927067A (en) * 1997-11-13 1999-07-27 United Technologies Corporation Self-cleaning augmentor fuel manifold
US20080134685A1 (en) * 2006-12-07 2008-06-12 Ronald Scott Bunker Gas turbine guide vanes with tandem airfoils and fuel injection and method of use
US7908863B2 (en) * 2008-02-12 2011-03-22 General Electric Company Fuel nozzle for a gas turbine engine and method for fabricating the same
US10077741B2 (en) 2012-05-29 2018-09-18 United Technologies Corporation Spraybar face seal retention arrangement
CN105546579A (zh) * 2015-12-25 2016-05-04 中国航空工业集团公司沈阳发动机设计研究所 一种燃油喷嘴
US11408610B1 (en) * 2021-02-03 2022-08-09 General Electric Company Systems and methods for spraying fuel in an augmented gas turbine engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB658294A (en) * 1948-09-02 1951-10-03 Power Jets Res & Dev Ltd Improvements in liquid fuel combustion apparatus
US2929201A (en) * 1954-05-20 1960-03-22 Armstrong Siddeley Motors Ltd Turbo jet engines as regards reheat
GB780493A (en) * 1954-07-20 1957-08-07 Rolls Royce Improvements relating to combustion equipment for gas-turbine engines
US2951341A (en) * 1956-09-19 1960-09-06 Westinghouse Electric Corp Fuel injection system for an aircraft engine
US2974488A (en) * 1956-11-27 1961-03-14 Snecma Combustion devices for continuous-flow internal combustion machines
US2949012A (en) * 1957-03-01 1960-08-16 Snecma Vaporisation burner device
US3102392A (en) * 1959-04-21 1963-09-03 Snecma Combustion equipment for jet propulsion units
US2963862A (en) * 1960-03-21 1960-12-13 Orenda Engines Ltd Fuel systems
FR1292404A (fr) * 1961-03-24 1962-05-04 Nord Aviation Grille d'injection multiple pour statoréacteur ou dispositif de post-combustion de turboréacteur
GB1212746A (en) * 1968-06-10 1970-11-18 Mini Of Technology Improvements in or relating to combustion devices
GB1255648A (en) * 1968-10-22 1971-12-01 Rolls Royce Duct burning system

Also Published As

Publication number Publication date
US4280324A (en) 1981-07-28
FR2404111B1 (un) 1982-03-26
FR2404111A1 (fr) 1979-04-20
DE2842047A1 (de) 1979-04-12

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee